Global Modeling of CO 2 Discharges with Aerospace Applications

Abstract

We developed a global model aiming to study discharges in CO 2 under various conditions, pertaining to a large spectrum of pressure, absorbed energy, and feeding values. Various physical conditions and form factors have been investigated. The model was applied to a case of radiofrequency discharge and to helicon type devices functioning in low and high feed conditions. In general, main charged species were found to be CO 2 + for sufficiently low pressure cases and O − for higher pressure ones, followed by CO 2 + , CO + , and O 2 + in the latter case. Dominant reaction is dissociation of CO 2 resulting into CO production. Electronegativity, important for radiofrequency discharges, increases with pressure, arriving up to 3 for high flow rates for absorbed power of 250 W, and diminishes with increasing absorbed power. Model results pertaining to radiofrequency type plasma discharges are found in satisfactory agreement with those available from an existing experiment. Application to low and high flow rates feedings cases of helicon thruster allowed for evaluation of thruster functioning conditions pertaining to absorbed powers from 50 W to 1.8 kW. The model allows for a detailed evaluation of the CO 2 potential to be used as propellant in electric propulsion devices.